Fixed-order dynamic compensation for a high-performance fighter aircraft
This paper presents a robust fixed-order dynamic compensator design for a high-performance fighter aircraft. The compensator design methodology is based on an approximate loop transfer recovery technique. Full-state gains are first designed for the dual system, which is the equivalent of designing a...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 1993-01, Vol.16 (1), p.104-110 |
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| container_end_page | 110 |
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| container_issue | 1 |
| container_start_page | 104 |
| container_title | Journal of guidance, control, and dynamics |
| container_volume | 16 |
| creator | BYRNS, EDWARD V. CALISE, ANTHONY J. |
| description | This paper presents a robust fixed-order dynamic compensator design for a high-performance fighter aircraft. The compensator design methodology is based on an approximate loop transfer recovery technique. Full-state gains are first designed for the dual system, which is the equivalent of designing a full-order observer. Then the loop characteristics at the dual system input are approximated with a compensator in controller canonical form. Finally, the optimal gains are implemented in the dual compensator to insure robustness and tracking performance at the plant output. The fixed-order dynamic compensator developed here is compared with a previously published full-order observer design. (Author) |
| doi_str_mv | 10.2514/3.11433 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 0731-5090 |
| ispartof | Journal of guidance, control, and dynamics, 1993-01, Vol.16 (1), p.104-110 |
| issn | 0731-5090 1533-3884 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_26056912 |
| source | Alma/SFX Local Collection |
| subjects | Aircraft performance Compensation Design techniques Fighter aircraft Military aircraft |
| title | Fixed-order dynamic compensation for a high-performance fighter aircraft |
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